[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

Dwivedi et al., 2019 - Google Patents

Aerodynamic characterization of bio inspired corrugated wings

Dwivedi et al., 2019

View PDF
Document ID
7727651734915263532
Author
Dwivedi Y
Bhargava V
Publication year
Publication venue
MOJ App Bio Biomech

External Links

Snippet

Wings of a dragon fly found in nature possess corrugations on its surface and known to exhibit efficient aerodynamic characteristics. In the present work, aerodynamic analysis of bio inspired profiles corrugated A, corrugated B and NACA 0010 were studied using 2-D …
Continue reading at www.academia.edu (PDF) (other versions)

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air-flow over aircraft surfaces, not otherwise provided for
    • B64C23/06—Influencing air-flow over aircraft surfaces, not otherwise provided for by generating vortices
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/10—Drag reduction
    • Y02T50/16—Drag reduction by influencing airflow
    • Y02T50/166—Drag reduction by influencing airflow by influencing the boundary layer
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2230/00—Boundary layer controls
    • B64C2230/12—Boundary layer controls by using electromagnetic tiles, fluid ionizers, static charges or plasma
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/44—Varying camber
    • B64C3/48—Varying camber by relatively-movable parts of wing structures
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2230/00—Boundary layer controls
    • B64C2230/22—Boundary layer controls by using a surface having multiple apertures of relatively small openings other than slots
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C21/00—Influencing air-flow over aircraft surfaces by affecting boundary-layer flow
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/10—Shape of wings
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/10—Drag reduction
    • Y02T50/16—Drag reduction by influencing airflow
    • Y02T50/162—Wing tip vortex reduction
    • Y02T50/164—Winglets
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2230/00—Boundary layer controls
    • B64C2230/02—Boundary layer controls by using acoustic waves generated by transducers

Similar Documents

Publication Publication Date Title
Goman et al. State-space representation of aerodynamic characteristics of an aircraft at high angles of attack
Watkins et al. Atmospheric winds and their implications for microair vehicles
von Karman et al. Airfoil theory for non-uniform motion
Srinivasan et al. Flowfield of a lifting rotor in hover-A Navier-Stokes simulation
Güzelbey et al. Numerical investigation of different airfoils at low Reynolds number in terms of aerodynamic performance of sailplanes by using XFLR5
Garmann et al. Three-dimensional flow structure and aerodynamic loading on a low aspect ratio, revolving wing
Dwivedi et al. Aerodynamic performance of micro aerial wing structures at low Reynolds number
Lian Numerical study of a flapping airfoil in gusty environments
Dwivedi et al. Aerodynamic characterization of bio inspired corrugated wings
Anuar et al. Aerodynamic Analysis of Unnamed Aerial Vehicle Serindit V-2 Using Computational Fluid Dynamics
Sharma An aerodynamic comparative analysis of airfoils for low-speed aircrafts
Sridhar et al. Effect of peak shape in bio inspired corrugated wing
Dwivedi Flow Field Study of Bio-Inspired Corrugated Airfoils at Low Reynolds Number with Different Peak Shapes
Roy et al. A Study of Model Separation Flow Behavior at High Angles of Attack Aerodynamics
Das et al. Aerodynamics of plunging airfoil in wind gust
Gopinathan et al. Passive flow control over NACA0012 aerofoil using vortex generators
Mehdi et al. Fluid Structure Interaction of Flow around a Pleated Insect 2D Airfoil at Ultra Low Reynolds Numbers
Asano et al. Control of Airfoil Flow at Cruise Condition by DBD Plasma Actuator-Sophisticated Airfoil vs. Simple Airfoil with Flow Control
Bhargava et al. Analysis of multi-element airfoil configurations: a numerical approach
Han et al. Investigation of the unsteady aerodynamic characteristics of an unmanned aerial vehicle with variable-sweep morphing
Lopes et al. Numerical and experimental study of a plunging airfoil
Altememe et al. Preliminary design and computational fluid dynamic analysis of flapping wing of micro aerial vehicle for low Reynolds numbers regime
Luo et al. A study on the aerodynamic characteristics of airfoil in the flapping adjustment stage during forward flight
Wang et al. Propulsive characteristics of twin oscillating airfoils
Moriche et al. Fast transverse maneuvers at low Reynolds numbers